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319.0 Aluminum vs. EN 1.4982 Stainless Steel

319.0 aluminum belongs to the aluminum alloys classification, while EN 1.4982 stainless steel belongs to the iron alloys. There are 31 material properties with values for both materials. Properties with values for just one material (4, in this case) are not shown. Please note that the two materials have significantly dissimilar densities. This means that additional care is required when interpreting the data, because some material properties are based on units of mass, while others are based on units of area or volume.

For each property being compared, the top bar is 319.0 aluminum and the bottom bar is EN 1.4982 stainless steel.

Metric UnitsUS Customary Units

Mechanical Properties

Brinell Hardness 78 to 84
230
Elastic (Young's, Tensile) Modulus, GPa 72
200
Elongation at Break, % 1.8 to 2.0
28
Fatigue Strength, MPa 76 to 80
420
Poisson's Ratio 0.33
0.28
Shear Modulus, GPa 27
76
Shear Strength, MPa 170 to 210
490
Tensile Strength: Ultimate (UTS), MPa 190 to 240
750
Tensile Strength: Yield (Proof), MPa 110 to 180
570

Thermal Properties

Latent Heat of Fusion, J/g 480
290
Maximum Temperature: Mechanical, °C 170
860
Melting Completion (Liquidus), °C 600
1430
Melting Onset (Solidus), °C 540
1390
Specific Heat Capacity, J/kg-K 880
470
Thermal Conductivity, W/m-K 110
13
Thermal Expansion, µm/m-K 22
16

Electrical Properties

Electrical Conductivity: Equal Volume, % IACS 27
2.3
Electrical Conductivity: Equal Weight (Specific), % IACS 84
2.7

Otherwise Unclassified Properties

Base Metal Price, % relative 10
22
Density, g/cm3 2.9
7.8
Embodied Carbon, kg CO2/kg material 7.7
4.9
Embodied Energy, MJ/kg 140
71
Embodied Water, L/kg 1080
150

Common Calculations

Resilience: Ultimate (Unit Rupture Work), MJ/m3 3.3 to 3.9
190
Resilience: Unit (Modulus of Resilience), kJ/m3 88 to 220
830
Stiffness to Weight: Axial, points 14
14
Stiffness to Weight: Bending, points 48
25
Strength to Weight: Axial, points 18 to 24
27
Strength to Weight: Bending, points 25 to 30
23
Thermal Diffusivity, mm2/s 44
3.4
Thermal Shock Resistance, points 8.6 to 11
17

Alloy Composition


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Aluminum (Al), % 85.8 to 91.5
0
Boron (B), % 0
0.0030 to 0.0090
Carbon (C), % 0
0.070 to 0.13
Chromium (Cr), % 0
14 to 16
Copper (Cu), % 3.0 to 4.0
0
Iron (Fe), % 0 to 1.0
61.8 to 69.7
Magnesium (Mg), % 0 to 0.1
0
Manganese (Mn), % 0 to 0.5
5.5 to 7.0
Molybdenum (Mo), % 0
0.8 to 1.2
Nickel (Ni), % 0 to 0.35
9.0 to 11
Niobium (Nb), % 0
0.75 to 1.3
Nitrogen (N), % 0
0 to 0.1
Phosphorus (P), % 0
0 to 0.040
Silicon (Si), % 5.5 to 6.5
0 to 1.0
Sulfur (S), % 0
0 to 0.030
Titanium (Ti), % 0 to 0.25
0
Vanadium (V), % 0
0.15 to 0.4
Zinc (Zn), % 0 to 1.0
0
Residuals, % 0 to 0.5
0